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    SYSTEM FOR REDUCING THE DYNAMIC BEHAVIOR OF THE MOVABLE SEGMENT OF A DEPLOYABLE NOZZLE FOR A ROCKET ENGINE
    3.
    发明申请
    SYSTEM FOR REDUCING THE DYNAMIC BEHAVIOR OF THE MOVABLE SEGMENT OF A DEPLOYABLE NOZZLE FOR A ROCKET ENGINE 有权
    用于减少用于发动机的可拆卸喷嘴的可移动部分的动态性能的系统

    公开(公告)号：US20140175191A1

    公开(公告)日：2014-06-26

    申请号：US14119648

    申请日：2012-05-15

    申请人： Noël David ,  Alain Pyre

    发明人： Noël David ,  Alain Pyre

    IPC分类号： F02K9/97

    CPC分类号： F02K9/976 ,  F05D2260/96 ,  F05D2300/433 ,  F05D2300/614

    摘要： A deployable nozzle for a rocket engine, the nozzle including at least a stationary divergent segment and a movable divergent segment that is coaxial about the stationary divergent segment and configured to move along the stationary divergent segment from a retracted position towards a deployed position. The deployable nozzle further includes a transverse stiffener that is prestressed in tension and that extends transversely relative to the movable divergent segment in a vicinity of a downstream end of the movable divergent segment between at least two points at a periphery of an inside wall of the movable divergent segment.

    摘要翻译： 一种用于火箭发动机的可展开的喷嘴，所述喷嘴包括至少一个固定的发散段和可移动的发散段，所述可分段与所述固定的发散段同轴并被配置成沿着所述固定的发散段从缩回位置向展开位置移动。 可展开的喷嘴还包括横向加强件，该横向加强件被预应力拉伸，并且在可移动发散段的下游端附近在可移动的发散段的下游端之间的至少两个点之间横向延伸， 发散段。

    Wrench with controlled tightening
    4.
    发明授权
    Wrench with controlled tightening 有权
    扳手带控制紧固

    公开(公告)号：US07036407B2

    公开(公告)日：2006-05-02

    申请号：US10806003

    申请日：2004-03-22

    申请人： Alain Pyre ,  Gilles Frechon ,  Pascal Coudrier ,  Ange-Marie Guillemin ,  Christian Roure

    发明人： Alain Pyre ,  Gilles Frechon ,  Pascal Coudrier ,  Ange-Marie Guillemin ,  Christian Roure

    IPC分类号： B24B23/14

    CPC分类号： B25B23/14

    摘要： The invention provides an electronic wrench which includes means for measuring the instantaneous applied torque and means for measuring the instantaneous angle of rotation during tightening. The physical parameters of the screw connection for tightening and a setpoint value for the tightening are initially entered into the wrench via a keypad. During the tightening operation, the processor means calculate the instantaneous traction force on the screw fastener as a function of the measured instantaneous values of torque and angle and as a function of the recorded characteristics of the screw fastener.

    摘要翻译： 本发明提供一种电子扳手，其包括用于测量瞬时施加的扭矩的装置和用于在紧固期间测量瞬时旋转角度的装置。 用于拧紧的螺丝连接的物理参数和紧固的设定值最初通过键盘输入到扳手中。 在紧固操作期间，处理器意味着根据所测量的扭矩和角度的瞬时值以及作为螺钉紧固件的记录特性的函数来计算螺丝紧固件上的瞬时牵引力。

    Static metal gasket and method of manufacturing it
    5.
    发明授权
    Static metal gasket and method of manufacturing it 有权
    静电金属垫片及其制造方法

    公开(公告)号：US06619668B1

    公开(公告)日：2003-09-16

    申请号：US09695728

    申请日：2000-10-23

    申请人： Alain Pyre

    发明人： Alain Pyre

    IPC分类号： F16J1502

    CPC分类号： F16J15/0887 ,  B21D53/20

    摘要： The metal static gasket forms an annular body about an axis ZZ′. The profile of the gasket in axial half-section presents an elongated S-shape and comprises a lateral first portion defining the inner peripheral surface of the gasket, a lateral second portion defining the outer peripheral surface of the gasket, said lateral first and second portions being offset from each other along the direction of the axis of the gasket. The gasket also presents a curved third portion of undulating shape having a substantially rectilinear first contact region at one of its ends, and a curved fourth portion of undulating shape having a substantially rectilinear second contact region at one of its end extending perpendicularly to the axis of the gasket in such a manner that the gasket provides sealing between two flanges solely by means of the axial pressure exerted by the flanges.

    摘要翻译： 金属静态垫圈围绕轴线ZZ'形成环形体。 衬垫在轴向半部分中的轮廓具有细长的S形并且包括限定垫圈的内周表面的横向第一部分，限定垫圈外周表面的横向第二部分，所述横向第一和第二部分 沿着垫圈的轴线的方向彼此偏移。 垫圈还呈现起伏形状的弯曲第三部分，其在其一端处具有基本上直线的第一接触区域，并且具有波形形状的弯曲第四部分，其具有基本上直线的第二接触区域，其一端处垂直于 垫圈以这样的方式使得垫圈仅通过由凸缘施加的轴向压力提供在两个凸缘之间的密封。

    System for reducing the dynamic behavior of the movable segment of a deployable nozzle for a rocket engine
    6.
    发明授权
    System for reducing the dynamic behavior of the movable segment of a deployable nozzle for a rocket engine 有权
    用于降低用于火箭发动机的可展开喷嘴的可动部分的动态特性的系统

    公开(公告)号：US09494110B2

    公开(公告)日：2016-11-15

    申请号：US14119648

    申请日：2012-05-15

    申请人： Noël David ,  Alain Pyre

    发明人： Noël David ,  Alain Pyre

    IPC分类号： F02K9/00 ,  F02K9/97

    CPC分类号： F02K9/976 ,  F05D2260/96 ,  F05D2300/433 ,  F05D2300/614

    摘要： A deployable nozzle for a rocket engine, the nozzle including at least a stationary divergent segment and a movable divergent segment that is coaxial about the stationary divergent segment and configured to move along the stationary divergent segment from a retracted position towards a deployed position. The deployable nozzle further includes a transverse stiffener that is prestressed in tension and that extends transversely relative to the movable divergent segment in a vicinity of a downstream end of the movable divergent segment between at least two points at a periphery of an inside wall of the movable divergent segment.

    摘要翻译： 一种用于火箭发动机的可展开的喷嘴，所述喷嘴包括至少一个固定的发散段和可移动的发散段，所述可分段与所述固定的发散段同轴并被配置成沿着所述固定的发散段从缩回位置向展开位置移动。 可展开的喷嘴还包括横向加强件，该横向加强件被预应力拉伸，并且在可移动发散段的下游端附近在可移动的发散段的下游端之间的至少两个点之间横向延伸， 发散段。